|
gptkbp:instance_of
|
gptkb:turbofan_engine
gptkb:hydroelectric_power_generation
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 700 ° C
|
|
gptkbp:capacity
|
8.5 MW
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:combustor_type
|
reverse flow
|
|
gptkbp:compressor_type
|
centrifugal compressor
|
|
gptkbp:configuration
|
turbo-shaft
|
|
gptkbp:control_system
|
mechanical control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_date
|
gptkb:Cold_War
|
|
gptkbp:design_feature
|
compact design
|
|
gptkbp:development
|
1950s to 1960s
|
|
gptkbp:elevation
|
2000 meters
|
|
gptkbp:emissions_standard
|
compliant with regulations
|
|
gptkbp:engine_configuration
|
single engine
various upgrades available
horizontal configuration
mounted on helicopter
|
|
gptkbp:engine_power
|
2000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:exhaust_system
|
tailpipe exhaust
|
|
gptkbp:first_flight
|
1950s
|
|
gptkbp:fuel_economy
|
good
variable
|
|
gptkbp:fuel_type
|
gptkb:gasoline
aviation kerosene
|
|
gptkbp:historical_significance
|
pioneering design in turboshaft technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Artouste IIIB
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:launch_window
|
electric starter
|
|
gptkbp:legacy
|
influenced future turboshaft designs
|
|
gptkbp:location
|
gptkb:France
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:SNECMA
|
|
gptkbp:market_segment
|
civil and military aviation
|
|
gptkbp:noise_level
|
moderate
|
|
gptkbp:notable_users
|
Alouette III
Alouette II
|
|
gptkbp:operational_range
|
varied by application
|
|
gptkbp:operational_since
|
gptkb:1959
|
|
gptkbp:operational_use
|
commercial and military operations
|
|
gptkbp:owner
|
gptkb:Électricité_de_France
|
|
gptkbp:part_of
|
Artouste hydroelectric complex
|
|
gptkbp:power_output
|
500 shp
|
|
gptkbp:propulsion
|
4.2:1
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
Artouste IIIC
|
|
gptkbp:turbine_blades
|
alloy material
|
|
gptkbp:turbine_type
|
Francis turbine
single-stage turbine
|
|
gptkbp:type
|
gptkb:reservoir
|
|
gptkbp:used_in
|
helicopters
|
|
gptkbp:vibration_level
|
low
|
|
gptkbp:water_source
|
Gave d' Ossau
|
|
gptkbp:weight
|
120 kg
|
|
gptkbp:bfsParent
|
gptkb:SA_315_Lama
|
|
gptkbp:bfsLayer
|
6
|